US3216215A - Temperature controlled incubator-hatchers - Google Patents

Temperature controlled incubator-hatchers Download PDF

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US3216215A
US3216215A US347819A US34781964A US3216215A US 3216215 A US3216215 A US 3216215A US 347819 A US347819 A US 347819A US 34781964 A US34781964 A US 34781964A US 3216215 A US3216215 A US 3216215A
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coolant
incubator
hatchers
evaporator
supply line
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Donald F Schuett
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CLIMATE Inc
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    • AHUMAN NECESSITIES
    • A01AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01KANIMAL HUSBANDRY; AVICULTURE; APICULTURE; PISCICULTURE; FISHING; REARING OR BREEDING ANIMALS, NOT OTHERWISE PROVIDED FOR; NEW BREEDS OF ANIMALS
    • A01K41/00Incubators for poultry
    • A01K41/02Heating arrangements
    • A01K41/023Devices for regulating temperature
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/2496Self-proportioning or correlating systems
    • Y10T137/2559Self-controlled branched flow systems
    • Y10T137/2574Bypass or relief controlled by main line fluid condition
    • Y10T137/2605Pressure responsive
    • Y10T137/2607With pressure reducing inlet valve

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  • This invention relates to incubator-hatchers in which eggs, usually of poultry or fowl, are incubated and hatched, and more particularly to the features thereof and in association therewith by which heat from any source, is carried oif so that the incubator-hatcher is maintained at the desired temperature.
  • incubator-hatching business has been one of the really large businesses in the food industry, and literally millions of eggs annually (often a million in a single hatchery) are placed in incubatorhatchers-a sort of box with various air-conditioning featuresfor incubation and hatching.
  • the desires for best conditioning of the air in such incubator-hatchers include proper humidity control, maintenance of proper carbon dioxide balance, air circulation, and of course temperature control-in a context wherein the eggs and :animals generate heat themselves that must be carried oif or disposed of in some manner. See as one example of prior thinking, Ross Patent 2,026,801.
  • the incubator-hatchers For example, many operators desire to maintain the incubator-hatchers at an average temperature of 991/2 degrees F. for incubating chicken eggs, or up to 99% degrees when the incubator is only partly filled. Temperature in the hatching compartment at the time of transfer is preferred by many such operators to be 981/2 degrees. Then at the end of the 21st day when the chicks are practically all hatched the temperature is often lowered to 97 degrees.
  • the group of incubator-hatchers in a bank may at times of day and climate and incubation load all be drawing little to no cooling and then all demand full load almost at once. And when the total average requirements of all the incubator-hatchers are perhaps half the capacity of the refrigeration unit, the individual incubator-hatchers place their loads upon the system at odd and nonsynchronized times, thus giving very rapid and frequent off-on cycling of the equipment with sharply varying loads--to an extent that conventional equipment has been found unsatisfactory for the purpose.
  • the motors burn out from too many starts and stops too close upon each other; the starter switches give trouble from too many operations; etc.
  • an object of this invention is to provide improved means for cooling a group of incubator-hatchers which is more reliable than conventional systems.
  • Other objects such as modest cost, operating expense, etc., are apparent from this description and the accompanying drawing wherein there is disclosed schematically one embodiment of an incubatorhatcher system in accordance with this invention.
  • a rst substantially conventional refrigeration system is used to cool a second coolant uid, which may conveniently be water.
  • This second coolant iluid is stored in sufficient quantity in the system that individual incubator-hatcher load changes dont draw down the water temperature excessively in either amount or speed of change; and also this coolant is continuously circulated to keep the water cooling eilicient and to serve some other purposes, among the most critical of which is:
  • the primary source of cooling which eventually winds up cooling the incubator-hatchers 3 and 4, may conveniently take the form of typical home refrigerator or air-conditioning systems schematically illustrated on the drawing as a pair of compressors 6a and 6b, discharging to a condenser coil 7 which is connected through an expansion valve 8 to a coil evaporator 9 from which the compressors 6a and 6b take suction.
  • a continuous delivery pump 11 which in turn discharges to a coolant supply line 12 (that may conveniently have a surge tank 12a therealong), and having several alternative discharge paths through which coolant may return back into the chiller tank 10.
  • a coolant by-pass line 13 in which may be located a pressure regulator valve 13a of a type designed to maintain constant pressure on the upstream side thereof.
  • This valve 13a is set to maintain a pressure just above the normal coolant supply pressure, for example 35 pounds, and whenever the pressure in that line exceeds 35 pounds the valve 13a opens and by-passes coolant directly back into the chiller tank 10, thus affording continuous operation of the pump 11 and avoiding off-on cycling of the pump, its motor and controls therefor. In one preferred operation there is always at least a little water passing through the bypass 13.
  • the other return paths from the coolant supply line 12 to the chiller tank 10 are in circuit-parallel with the by-pass 13, but each is a return through a different incubator-hatcher to afford controlled cooling thereto.
  • each incubator-hatcher there may be provided for each incubator-hatcher a pressure reducing valve 14 connected to the coolant supply 12, though in some system designs these pressure reducers 14 at this location are not necessary.
  • a valve 15 responsive to temperature in its corresponding incubator-hatcher Receiving coolant at a constant pressure from each such pressure reducing valve 14, is a valve 15 responsive to temperature in its corresponding incubator-hatcher. Any one of several thermostatically controlled valves on the market are convenient for this application, and the temperature responsive element 15a, commonly of thermostatic design, may be located in the incubator-hatcher at any one of several locations, as for example on the side wall perhaps half way between floor and ceiling of the incubator-hatcher.
  • Cooling heat exchange means are provided in each of the incubator-hatchers, and in the embodiment illustrated this cooling heat exchange means takes the lform of a coil of pipe or tubing illustrated at 16 and deriving its coolant from the thermo-responsive valve 15.
  • the various cooling heat exchange means 16 discharge coolant into a warm coolant return line 17, thence back into the chiller tank 10.
  • the combination of the chiller tank and coil 9 evaporator is a heat exchange unit by which the refrigerant of the compressor system 6, 7, 8 and 9 draws heat from the coolant in the pump system 10, 11, 12, 13, 14, 15, 16, 17.
  • Other forms of heat exchangers may be used here, but there are significant advantageous features to the coil-9-in-tank-10 arrangement.
  • the return coolant is adapted to agitate the coolant water in tank 10 for more efficient heat transfer from the coil 9.
  • the surplus of coolant in the tank which serves as storage serves also to absorb the thermal shock of any sudden return of warm coolant when one or two or ten incubator-hatchers take load simultaneously and the by-pass 13 is suddenly shut off by valve 13a. This absorbtion of thermal shock prevents false-start cycling of the compressors which respond directly or indirectly to evaporator temperature and to coolant temperature in tank 10.
  • inlet temperature at the time one incubator-hatcher first cuts on may cause the second compressor to start unnecessarily and run for only a minute and then cut off again with resultant unnecessary wear and inefficiency that is avoided by the action of the cool water reservoir of tank 10 receiving the return warmed coolant.
  • the function -of the reservoir of cold secondary coolant is similar t0 a heat or temperature surge tank: It smoothes out the temperature variations, with resultant reduction in off-on cycling and increase in several factors of efficiency.
  • Some of this desired function can be accomplished with structures other than an evaporator coil of primary refrigerant inside a tank of secondary coolant--as for example, a relatively large volume vessel or conduit can receive the return warm coolant and mix it with other by-pass and return coolant before any of it is fed to a heat exchanger to give up heat to the primary refrigerant-but the coil-evaporator-in-coolant-tank arrangement is easy to design and build and works well.
  • the primary refrigeration system 6, 7, 8, 9 must of course be temperature responsive to the coolant in the In many installations the secondary coolant is found to be best maintained at 55 F. though the equipment should carry adjustability of this temperature at least to ten degrees on either side of 55.
  • Various designs and locations of temperature responsive means (not shown), by which the compressors 6a and 6b are rendered responsive directly or indirectly to the temperature of the coolant in the secondary system, may be used.
  • the best thermal surge tank function is obtained when the coolant temperature responsive control for the compressors is not located immediately adjacent the coil evaporator 9 or the inlet for coolant return.
  • temperature responsive control is located even downstream of the pump 11, thereby to slow the compressor response to sudden surges Iof warm return coolant and reduce the cycling of the compressors 6a and 6b.
  • a surge tank or accumulator may be added to the primary refrigeration system 6, 7, 8, 9 or deleted from the secondary cooling system 10, 11, 12, 13, 14, 15, 16, 17. Some may even sacrifice good individual temperature control by putting two incubators in series of a coolant path, instead of all of the incubators in parallel as is preferred.
  • a coolant by-pass having pressure responsive means therein and connected between said coolant supply line and said chiller tank whereby coolant is discharged :from said coolant supply line into said chiller tank whenever the pressure in said coolant supply line execeeds a predetermined level;
  • a pressure reducing device connected to receive coolant from said coolant supply line and to discharge such coolant at a desired pressure
  • heat exchange means located in said incubatorhatcher and connected to receive coolant from said valve means, whereby said coolant may be brought to absorb heat from said incubatorhatcher;
  • said evaporator being part of a heat exchange unit by which a secondary coolant fluid is cooled;
  • a coolant by-pass connected between said coolant supply line and said heat exchange unit whereby coolant is discharged :from said coolant supply line into said heat exchange unit whenever the discharge pressure of said pump exceeds a predetermined level;
  • a valve means responsive to temperature in said incubator-hatcher and connected to receive coolant from said coolant supply line;
  • heat exchange means located in said incubatorhatcher and connected to receive coolant from said valve means, whereby said coolant may be brought to absorb heat from said incubatorhatcher;
  • warm coolant return conduit connected to receive coolant from all such heat exchange means in incubator-hatchers and return it to said heat exchange unit.
  • a chiller adapted to hold coolant uid and constituting with said evaporator a chiller heat exchange unit by which said coolant fluid is cooled;
  • each incubator-hatcher being connected to receive amounts of said coolant varying in response to the temperature in ⁇ said incubator-hatcher and to discharge warmed coolant back to said chiller tank, whereby said incubator-hatcher is cooled whenever its temperature exceeds a predetermined setting;
  • coolant by-pass means in circuit parallel with said cooling heat exchange means located in each incubator-hatcher, said coolant by-pass means being connected to by-pass coolant from the upstream side to the downstream side of said cooling heat exchange means whenever the pressure differential thereacross exceeds a predetermined value;
  • pump means adapted continuously to move coolant in the coolant circuit comprising said chiller heat exchange unit wherein the coolant gives up its heat and the circuit parallel connection of said by-pass and the incubator-hatchers where the coolant absorbs heat from the incubator-hatchers.
  • a system of incubator-hatchers and related cooling apparatus comprising the combination of:
  • refrigeration apparatus including a compressor, a condenser for giving up heat, an evaporator heat exchanger for absorbing heat from a coolant iluid;
  • a coolant fluid system comprising said evaporator heat exchanger
  • a continuous running pump which takes continuous suction on the coolant uid cooled in the evaporator heat exchanger and discharges it continuously;
  • each of lsaid coils in a different one among a plurality of incubator-hatchers, whereby said coils receive cooled coolant fluid ow variably therethrough in response to temperature variations in the incubator-hatcher to cool such incubator-hatch- ⁇ a by-pass line in parallel with said plurality of incubator-hatchers for receiving coolant from said pump and, by-passing that portion of the pumps discharge not required by said incubatorhatchers back into the evaporator heat exchanger, whereby the continuous running pumps discharge may be maintained at approximately constant pressure even when different cooling coils are cutting off and on in response to temperature variations in their respective incubatorhatchers;

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Description

Nov. 9, 1965 D. F. scHUETT 3,216,215
TEMPERATURE CONTROLLED INCUBATOR-HATCHERS Filed Feb. 27, 1964 5000/0/ /C Jcaez INVENTOR BY MMQL@ Z United States Patent M 3,216,215 TEMPERATURE CONTROLLED lNCUBATR-HATCHERS Donald F. Schuett, Climate Inc., P.0. Box 932, Austin, Tex. Filed Feb. 27, 1964, Ser. No. 347,819 4 Claims. (Cl. 62-185)` This invention relates to incubator-hatchers in which eggs, usually of poultry or fowl, are incubated and hatched, and more particularly to the features thereof and in association therewith by which heat from any source, is carried oif so that the incubator-hatcher is maintained at the desired temperature.
For many years now the incubator-hatching business has been one of the really large businesses in the food industry, and literally millions of eggs annually (often a million in a single hatchery) are placed in incubatorhatchers-a sort of box with various air-conditioning featuresfor incubation and hatching. The desires for best conditioning of the air in such incubator-hatchers include proper humidity control, maintenance of proper carbon dioxide balance, air circulation, and of course temperature control-in a context wherein the eggs and :animals generate heat themselves that must be carried oif or disposed of in some manner. See as one example of prior thinking, Ross Patent 2,026,801.
The common practice for years has been to assemble a bank or a group of these incubator-hatchers in close proximity to each other, each ot' a size determined by factors not germane to this invention, but each requiring for best results, accurate temperature control, which is a subject of this invention.
For example, many operators desire to maintain the incubator-hatchers at an average temperature of 991/2 degrees F. for incubating chicken eggs, or up to 99% degrees when the incubator is only partly filled. Temperature in the hatching compartment at the time of transfer is preferred by many such operators to be 981/2 degrees. Then at the end of the 21st day when the chicks are practically all hatched the temperature is often lowered to 97 degrees.
These temperatures must be maintained with tolerable accuracy, without upsetting the carbon -dioxide balance in the air, the humidity or the like, and these considerations in combination with cost considerations rule out conventional air-conditioning systems as highly unpreferred. But a further more fundamental engineering problem has plagued the many who sought to air-condition a bank of incubator-hatchers with ordinary airconditioning equipment:
The group of incubator-hatchers in a bank, may at times of day and climate and incubation load all be drawing little to no cooling and then all demand full load almost at once. And when the total average requirements of all the incubator-hatchers are perhaps half the capacity of the refrigeration unit, the individual incubator-hatchers place their loads upon the system at odd and nonsynchronized times, thus giving very rapid and frequent off-on cycling of the equipment with sharply varying loads--to an extent that conventional equipment has been found unsatisfactory for the purpose. The motors burn out from too many starts and stops too close upon each other; the starter switches give trouble from too many operations; etc.
And many of these units are used in relatively out of the way places where service is slow to come by and thousands of dollars Worth of eggs or baby chickens or turkeys may be lost while waiting on service.
As a result of these and other problems the vast majority of systems in use today use fresh water supplies 3,2 l 6,2 l 5 Patented Nov. 9, 1965 for cooling purposes, wastefully discarding the warmed water after use.
Thus in the air-conditioning of the incubator-hatchers is found the combination of an acute need for reliability of the equipment together with extreme lload variation patterns that place demands on the equipment beyond conventional equipments capacity to handle with the required reliability.
lt is this special need for extra reliability in this context of extra heavy demands upon the equipment by virtue of the peculiarly frequent and extent load variations, that brought applicant to undertake the labors that eventually resulted in this invention.
Accordingly, it is apparent that an object of this invention is to provide improved means for cooling a group of incubator-hatchers which is more reliable than conventional systems. Other objects such as modest cost, operating expense, etc., are apparent from this description and the accompanying drawing wherein there is disclosed schematically one embodiment of an incubatorhatcher system in accordance with this invention.
These objects are accomplished in accordance with this invention by arranging for cooling of the bank of incubator-hatchers not with the primary refrigerant, like the Freon in an office or home air-conditioning system or refrigerator, as does for example, Hoffmann 1,782,688 and Hoffmann 2,522,948.
Rather, in accordance with this invention a rst substantially conventional refrigeration system is used to cool a second coolant uid, which may conveniently be water. This second coolant iluid is stored in sufficient quantity in the system that individual incubator-hatcher load changes dont draw down the water temperature excessively in either amount or speed of change; and also this coolant is continuously circulated to keep the water cooling eilicient and to serve some other purposes, among the most critical of which is:
Neither the compressors nor the machinery for moving the incubator-hatcher coolant iluid cycles with every incubator-hatcher load change. In accordance with this invention, the problem-producing frequent-cycling of motors and compressors or pumps is solved by valving of continuous moving coolant, rather than by off-on cycling.
The invention is best understood by reference to the drawing which discloses one exemplar of a system incorporating the invention.
The beginning of a series of incubator-hatchers is illustarted simply as boxes 3 and 4. Access doors, drip pans, air circulation means, humidity control means (which may be aixed to the cold water system of this invention) and other such details are not illustrated since they are not a part of this invention. And while the boxes illustrated are numbered 3 and 4, it is of course understood that there may be others in the same system, six to a hundred such units being not uncommon numbers for inclusion in a single cooling system.
The primary source of cooling Which eventually winds up cooling the incubator- hatchers 3 and 4, may conveniently take the form of typical home refrigerator or air-conditioning systems schematically illustrated on the drawing as a pair of compressors 6a and 6b, discharging to a condenser coil 7 which is connected through an expansion valve 8 to a coil evaporator 9 from which the compressors 6a and 6b take suction.
Since at various times and circumstances the system needs on the order of half the capacity that is required for total peak loads, the use of two appropriately sized compressors instead of one large one, affords greater efficiency as well as a stand-by minimum operating capacity should one compressor or its controls be temporarily disabled. More important, it reduces the number of on-off cycles which any given motor or compressor or the controls therefor must go through in any years operation, thereby increasing the reliability of the system by reducing the demands which off-on cycling present.
'charging into a continuous delivery pump 11, which in turn discharges to a coolant supply line 12 (that may conveniently have a surge tank 12a therealong), and having several alternative discharge paths through which coolant may return back into the chiller tank 10.
One of those return paths is through a coolant by-pass line 13 in which may be located a pressure regulator valve 13a of a type designed to maintain constant pressure on the upstream side thereof. This valve 13a is set to maintain a pressure just above the normal coolant supply pressure, for example 35 pounds, and whenever the pressure in that line exceeds 35 pounds the valve 13a opens and by-passes coolant directly back into the chiller tank 10, thus affording continuous operation of the pump 11 and avoiding off-on cycling of the pump, its motor and controls therefor. In one preferred operation there is always at least a little water passing through the bypass 13.
The other return paths from the coolant supply line 12 to the chiller tank 10 are in circuit-parallel with the by-pass 13, but each is a return through a different incubator-hatcher to afford controlled cooling thereto.
Thus, there may be provided for each incubator-hatcher a pressure reducing valve 14 connected to the coolant supply 12, though in some system designs these pressure reducers 14 at this location are not necessary.
Receiving coolant at a constant pressure from each such pressure reducing valve 14, is a valve 15 responsive to temperature in its corresponding incubator-hatcher. Any one of several thermostatically controlled valves on the market are convenient for this application, and the temperature responsive element 15a, commonly of thermostatic design, may be located in the incubator-hatcher at any one of several locations, as for example on the side wall perhaps half way between floor and ceiling of the incubator-hatcher.
Cooling heat exchange means are provided in each of the incubator-hatchers, and in the embodiment illustrated this cooling heat exchange means takes the lform of a coil of pipe or tubing illustrated at 16 and deriving its coolant from the thermo-responsive valve 15.
The various cooling heat exchange means 16 discharge coolant into a warm coolant return line 17, thence back into the chiller tank 10.
It is apparent that the combination of the chiller tank and coil 9 evaporator is a heat exchange unit by which the refrigerant of the compressor system 6, 7, 8 and 9 draws heat from the coolant in the pump system 10, 11, 12, 13, 14, 15, 16, 17. Other forms of heat exchangers may be used here, but there are significant advantageous features to the coil-9-in-tank-10 arrangement.
Preferably the return coolant is adapted to agitate the coolant water in tank 10 for more efficient heat transfer from the coil 9. The surplus of coolant in the tank which serves as storage, serves also to absorb the thermal shock of any sudden return of warm coolant when one or two or ten incubator-hatchers take load simultaneously and the by-pass 13 is suddenly shut off by valve 13a. This absorbtion of thermal shock prevents false-start cycling of the compressors which respond directly or indirectly to evaporator temperature and to coolant temperature in tank 10.
In the absence of this tank-of-secondary-coolant-Withcoil-of-primary-refrigerant-arrangement, or some reasonable equivalent thereof, a minor change in warm coolant ysecondary system 10, 11, 12, 13, 14, 15, 16, 17.
inlet temperature at the time one incubator-hatcher first cuts on may cause the second compressor to start unnecessarily and run for only a minute and then cut off again with resultant unnecessary wear and inefficiency that is avoided by the action of the cool water reservoir of tank 10 receiving the return warmed coolant.
The function -of the reservoir of cold secondary coolant, is similar t0 a heat or temperature surge tank: It smoothes out the temperature variations, with resultant reduction in off-on cycling and increase in several factors of efficiency. Some of this desired function can be accomplished with structures other than an evaporator coil of primary refrigerant inside a tank of secondary coolant--as for example, a relatively large volume vessel or conduit can receive the return warm coolant and mix it with other by-pass and return coolant before any of it is fed to a heat exchanger to give up heat to the primary refrigerant-but the coil-evaporator-in-coolant-tank arrangement is easy to design and build and works well.
The primary refrigeration system 6, 7, 8, 9 must of course be temperature responsive to the coolant in the In many installations the secondary coolant is found to be best maintained at 55 F. though the equipment should carry adjustability of this temperature at least to ten degrees on either side of 55. Various designs and locations of temperature responsive means (not shown), by which the compressors 6a and 6b are rendered responsive directly or indirectly to the temperature of the coolant in the secondary system, may be used.
However, the best thermal surge tank function is obtained when the coolant temperature responsive control for the compressors is not located immediately adjacent the coil evaporator 9 or the inlet for coolant return. Preferably that temperature responsive control is located even downstream of the pump 11, thereby to slow the compressor response to sudden surges Iof warm return coolant and reduce the cycling of the compressors 6a and 6b.
Modifications may be made in and additions may be added to the structure above described for exemplary purposes without departure from the scope of the invention. For example, it will be normal to add a water make-up inlet, perhaps opening into the chiller tank to make up any water that may be lost through leaking from the normally closed system, or through use of coolant water by humidifier systems that may be appended thereto. Or the by-pass 13 may be connected from the far end of the coolant supply 12 so that circulation through the by-pass also passes through the entirety of the coolant supply to keep the coolant from warming excessively in some portion of the coolant supply line 12 that becomes dead-end for a While during an off load of the nearby incubator-hatchers. Or depending upon design a surge tank or accumulator may be added to the primary refrigeration system 6, 7, 8, 9 or deleted from the secondary cooling system 10, 11, 12, 13, 14, 15, 16, 17. Some may even sacrifice good individual temperature control by putting two incubators in series of a coolant path, instead of all of the incubators in parallel as is preferred.
Accordingly, the foregoing description is to be considered as illustrative only, and is not to be construed as a continuous running pump taking suction upon the coolant in said chiller tank and discharging to a coolant supply line;
a coolant by-pass having pressure responsive means therein and connected between said coolant supply line and said chiller tank whereby coolant is discharged :from said coolant supply line into said chiller tank whenever the pressure in said coolant supply line execeeds a predetermined level;
for each of said incubator-hatchers a pressure reducing device connected to receive coolant from said coolant supply line and to discharge such coolant at a desired pressure,
a valve means responsive to temperature in said incubator-hatcher connected to receive coolant from said pressure reducing device;
heat exchange means located in said incubatorhatcher and connected to receive coolant from said valve means, whereby said coolant may be brought to absorb heat from said incubatorhatcher;
and warm coolant return conduit connected to receive coolant from all such heat exchange means and return it to said chiller tank.
2. In `a system of a plurality of incubator-hatchers having a cooling heat exchange means therein and related cooling heat exchange means therein and related cooling apparatus including a compressor, condenser and evaporator adapted to have refrigerant circulated therethrough to cool said evaporator, the combination therewith of features as follows:
said evaporator being part of a heat exchange unit by which a secondary coolant fluid is cooled;
a continuous delivery pump taking suction upon the coolant in said heat exchange unit and discharging to a coolant supply line;
a coolant by-pass connected between said coolant supply line and said heat exchange unit whereby coolant is discharged :from said coolant supply line into said heat exchange unit whenever the discharge pressure of said pump exceeds a predetermined level;
for each of said incubator-hatchers a valve means responsive to temperature in said incubator-hatcher and connected to receive coolant from said coolant supply line;
heat exchange means located in said incubatorhatcher and connected to receive coolant from said valve means, whereby said coolant may be brought to absorb heat from said incubatorhatcher;
and warm coolant return conduit connected to receive coolant from all such heat exchange means in incubator-hatchers and return it to said heat exchange unit.
3. In a system of a plurality of incubator-hatchers each having a cooling heat exchange means therein and related cooling apparatus including a compressor, condenser and evaporator adapted to have refrigerant circulated therethrough to cool said evaporator, the combination therewith yof features as follows:
a chiller adapted to hold coolant uid and constituting with said evaporator a chiller heat exchange unit by which said coolant fluid is cooled;
the cooling hea-t exchange means located in each incubator-hatcher being connected to receive amounts of said coolant varying in response to the temperature in `said incubator-hatcher and to discharge warmed coolant back to said chiller tank, whereby said incubator-hatcher is cooled whenever its temperature exceeds a predetermined setting; v
a coolant by-pass means in circuit parallel with said cooling heat exchange means located in each incubator-hatcher, said coolant by-pass means being connected to by-pass coolant from the upstream side to the downstream side of said cooling heat exchange means whenever the pressure differential thereacross exceeds a predetermined value;
and pump means adapted continuously to move coolant in the coolant circuit comprising said chiller heat exchange unit wherein the coolant gives up its heat and the circuit parallel connection of said by-pass and the incubator-hatchers where the coolant absorbs heat from the incubator-hatchers.
4. A system of incubator-hatchers and related cooling apparatus comprising the combination of:
refrigeration apparatus including a compressor, a condenser for giving up heat, an evaporator heat exchanger for absorbing heat from a coolant iluid;
a coolant fluid system comprising said evaporator heat exchanger,
a continuous running pump which takes continuous suction on the coolant uid cooled in the evaporator heat exchanger and discharges it continuously;
a plurality of cooling coils connected to receive coolant from said pump and to discharge back into the evaporator heat exchanger, each of lsaid coils in a different one among a plurality of incubator-hatchers, whereby said coils receive cooled coolant fluid ow variably therethrough in response to temperature variations in the incubator-hatcher to cool such incubator-hatch- `a by-pass line in parallel with said plurality of incubator-hatchers for receiving coolant from said pump and, by-passing that portion of the pumps discharge not required by said incubatorhatchers back into the evaporator heat exchanger, whereby the continuous running pumps discharge may be maintained at approximately constant pressure even when different cooling coils are cutting off and on in response to temperature variations in their respective incubatorhatchers;
whereby cooled coolant fluid is being continuously circulated from the evaporator heat exchanger back again to the evaporator heat exchanger through one or more among the by-pass and the various cooling coils connected to the pump discharge.
References Cited by the Examiner UNITED STATES PATENTS FOREIGN PATENTS 1l/33 Germany.
2/ 50 Switzerland.
WILLIAM I. WYE, Primary Examiner.
UNITED STATES PATENT OFFICE CERTIFICATE 0F CORRECTION Patent No 3 216,215 November 9, 1965 Donald F. Schuett e above numbered pat- It is hereby certified that error appears in th Patent should read as ent requiring correction and that the said Letters corrected below.
line 11, for "extent" read extreme Column 5, lines 26 and 27, heat exchange means therein".
Signed and sealed thS 2nd day of August 1966.
(SEAL) Attest:
EDWARD I. BRENNER ERNEST W. SWIDER Commissioner of Patents Attesting Officer

Claims (1)

1. IN A SYSTEM OF A PLURALITY OF INCUBATOR-HATCHERS EACH HAVING A COOLING HEAT EXCHANGE MEANS THEREIN AND RELATED COOLING APPARATUS INCLUDING A COMPRESSOR, CONDENSER, AND EVAPORATOR ADAPTED TO HAVE REFRIGERANT CIRCULATED THERETHROUGH TO COOL SAID EVAPORATOR, THE COMBINATION THEREWITH A FEATURES AS FOLLOWS: SAID EVAPORATOR BEING LOCATED IN A CHILLER TANK ADAPTED TO HOLD A SUPPLY OF COLLANT FLUID WHEREBY SAID EVAPORATOR OPERATES A COOL SAID COOLANT FLUID; A CONTINUOUS RUNNING PUMP TAKING SUCTION UPON THE COOLANT IN SAID CHILLER TANK AND DISCHARGING TO A COOLANT SUPPLY LINE; A COOLANT BY-PASS HAVING PRESSURE RESPONSIVE MEANS THEREIN AND CONNECTED BETWEEN SAID COOLANT SUPPLY LINE AND SAID CHILLER TANK WHEREBY COOLANT IS DISCHARGED FROM SAID COOLANT SUPPLY LINE INTO SAID CHILLER TANK WHENEVER THE PRESSURE IN SAID COOLANT SUPPLY LINE EXECEEDS A PREDETERMINED LEVEL; FOR EACH OF SAID INCUBATOR-HATCHERS A PRESSURE REDUCING DEVICE CONNECTED TO RECEIVE COOLANT FROM SAID COOLANT SUPPLY LINE AND TO
US347819A 1964-02-27 1964-02-27 Temperature controlled incubator-hatchers Expired - Lifetime US3216215A (en)

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Cited By (26)

* Cited by examiner, † Cited by third party
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WO1985001097A1 (en) * 1983-08-26 1985-03-14 Gilbertson Thomas A Pressurized, ice-storing chilled water system
US5099657A (en) * 1991-01-09 1992-03-31 Huang Chia Tsai Structure of cooling tank for water cooler
US5491982A (en) * 1994-10-27 1996-02-20 Aec, Inc. Chiller bypass
US5513500A (en) * 1993-11-26 1996-05-07 Daimler-Benz Aerospace Airbus Gmbh System for cooling food in an airplane
US5706883A (en) * 1996-08-09 1998-01-13 Jack M. Berry, Inc. Mass storage and dispensing system for liquids such as citrus products
US5784893A (en) * 1994-03-30 1998-07-28 Kabushiki Kaisha Toshiba Air conditioning system with built-in intermediate heat exchanger with two different types of refrigerants circulated
US5797271A (en) * 1996-04-23 1998-08-25 Pelican Bait, Inc Mobile brine tank quick-freezing system and method
WO1999019679A1 (en) * 1997-10-09 1999-04-22 Warren John S Modular temperature maintaining food receptacle system
US6012298A (en) * 1995-02-27 2000-01-11 Sunwell Engineering Company Limited Ice slurry delivery system
US6131398A (en) * 1995-11-07 2000-10-17 Alfa Laval Agri Ab Apparatus and method for cooling a product
US6185951B1 (en) * 1999-07-06 2001-02-13 In-Store Products Ltd. Temperature controlled case
NL1019949C2 (en) * 2002-02-12 2003-08-21 Henricus Gerardus Hermanus Pas Incubator with heat pipes.
US6832504B1 (en) 2003-11-19 2004-12-21 Be Intellectual Property, Inc. Liquid sensing system for an aircraft galley cooler using a two phase working fluid
US6845627B1 (en) 2003-11-10 2005-01-25 Be Intellectual Property, Inc. Control system for an aircraft galley cooler
US20050066679A1 (en) * 2003-09-30 2005-03-31 Boyer Jack Clyde Distributed operator cooling system
US6880351B2 (en) * 2001-09-05 2005-04-19 Be Intellectual Property, Inc. Liquid galley refrigeration system for aircraft
US20050210910A1 (en) * 2004-03-29 2005-09-29 Rigney Richard N Cooling system for a commercial aircraft galley
US20060053831A1 (en) * 2004-09-10 2006-03-16 Serge Dube Evaporation circuit for alternative refrigerant in a refrigeration system
US20070068187A1 (en) * 2005-09-26 2007-03-29 Gaetan Lesage Dual refrigerant refrigeration system and method
US20080092575A1 (en) * 2006-10-23 2008-04-24 Ralph Muscatell Solar air conditioning system
US20080134703A1 (en) * 2003-12-30 2008-06-12 Thomas Scherer Cooling System For Cooling Heat-Generating Installations and For Maintaining the Temperature of Closed-Off Areas at Below Cabin Temperature in an Aircraft
US7721797B2 (en) 2005-04-25 2010-05-25 Be Intellectual Property, Inc. Refrigerator-oven combination for an aircraft galley food service system
US8292192B1 (en) 2008-07-01 2012-10-23 The United States Of America As Represented By The Secretary Of Agriculture Variable stage humidity control system for poultry hatcheries
US20170142939A1 (en) * 2015-11-24 2017-05-25 Incubation Systems, Inc. Egg incubator conversion kit
US10040556B2 (en) 2013-10-07 2018-08-07 B/E Aerospace, Inc. Chilled air plenum system for aircraft galleys
US20240278623A1 (en) * 2023-02-17 2024-08-22 GM Global Technology Operations LLC Multimodal cooling systems including integrated cooling devices with refrigerant-to-coolant heat exchangers

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US1044444A (en) * 1912-06-27 1912-11-12 Allis Chalmers Fluid-pressure regulator.
DE588566C (en) * 1930-03-26 1933-11-28 Freundlich Maschinenfabrik A Cooling system, the cold use points of which are supplied with cold from a cold generating point by a cold carrier and in which a cold storage unit is available for all cold use points
US2237304A (en) * 1937-04-01 1941-04-08 Barber Colman Co Control for conditioning systems and the like
US2516508A (en) * 1946-12-26 1950-07-25 Curtiss Wright Corp Hydraulic system and valve therefor
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Cited By (53)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1985001097A1 (en) * 1983-08-26 1985-03-14 Gilbertson Thomas A Pressurized, ice-storing chilled water system
US5099657A (en) * 1991-01-09 1992-03-31 Huang Chia Tsai Structure of cooling tank for water cooler
US5513500A (en) * 1993-11-26 1996-05-07 Daimler-Benz Aerospace Airbus Gmbh System for cooling food in an airplane
US5784893A (en) * 1994-03-30 1998-07-28 Kabushiki Kaisha Toshiba Air conditioning system with built-in intermediate heat exchanger with two different types of refrigerants circulated
US5491982A (en) * 1994-10-27 1996-02-20 Aec, Inc. Chiller bypass
US6012298A (en) * 1995-02-27 2000-01-11 Sunwell Engineering Company Limited Ice slurry delivery system
US6301904B1 (en) 1995-02-27 2001-10-16 Sunwell Engineering Company Limited Ice slurry delivery system
US6131398A (en) * 1995-11-07 2000-10-17 Alfa Laval Agri Ab Apparatus and method for cooling a product
US5797271A (en) * 1996-04-23 1998-08-25 Pelican Bait, Inc Mobile brine tank quick-freezing system and method
US5706883A (en) * 1996-08-09 1998-01-13 Jack M. Berry, Inc. Mass storage and dispensing system for liquids such as citrus products
WO1999019679A1 (en) * 1997-10-09 1999-04-22 Warren John S Modular temperature maintaining food receptacle system
US5921096A (en) * 1997-10-09 1999-07-13 Warren; John S. Modular temperature maintaining food receptacle system
US6185951B1 (en) * 1999-07-06 2001-02-13 In-Store Products Ltd. Temperature controlled case
US8495887B2 (en) 2001-09-05 2013-07-30 Be Aerospace, Inc. Liquid galley refrigeration system for aircraft
US8151582B2 (en) * 2001-09-05 2012-04-10 Be Aerospace, Inc. Liquid galley refrigeration system for aircraft
US7421849B2 (en) 2001-09-05 2008-09-09 Be Intellectual Property, Inc. Liquid galley refrigeration system for aircraft
US20080289800A1 (en) * 2001-09-05 2008-11-27 Be Intellectual Property, Inc. Liquid galley refrigeration system for aircraft
US20070084226A1 (en) * 2001-09-05 2007-04-19 George Simadiris Liquid galley refrigeration system for aircraft
US6880351B2 (en) * 2001-09-05 2005-04-19 Be Intellectual Property, Inc. Liquid galley refrigeration system for aircraft
US20050178908A1 (en) * 2001-09-05 2005-08-18 George Simadiris Liquid galley refrigeration system for aircraft
US8813513B2 (en) 2001-09-05 2014-08-26 B/E Aerospace, Inc. Liquid galley refrigeration system for aircraft
US7137264B2 (en) 2001-09-05 2006-11-21 Be Intellectual Property, Inc. Liquid galley refrigeration system for aircraft
EP1334658A3 (en) * 2002-02-12 2004-01-02 Henricus Gerardus Hermanus Maria Pas Hatching machine with heat pipes
NL1019949C2 (en) * 2002-02-12 2003-08-21 Henricus Gerardus Hermanus Pas Incubator with heat pipes.
US20050066679A1 (en) * 2003-09-30 2005-03-31 Boyer Jack Clyde Distributed operator cooling system
US6845627B1 (en) 2003-11-10 2005-01-25 Be Intellectual Property, Inc. Control system for an aircraft galley cooler
US6832504B1 (en) 2003-11-19 2004-12-21 Be Intellectual Property, Inc. Liquid sensing system for an aircraft galley cooler using a two phase working fluid
US20080134703A1 (en) * 2003-12-30 2008-06-12 Thomas Scherer Cooling System For Cooling Heat-Generating Installations and For Maintaining the Temperature of Closed-Off Areas at Below Cabin Temperature in an Aircraft
US7784289B2 (en) * 2003-12-30 2010-08-31 Airbus Deutschland Gmbh Cooling system for cooling heat-generating installations and for maintaining the temperature of closed-off areas at below cabin temperature in an aircraft
WO2005094346A3 (en) * 2004-03-29 2007-11-15 Be Intellectual Pty Inc Improved cooling system for a commercial aircraft galley
JP2007537077A (en) * 2004-03-29 2007-12-20 ビーイー・インテレクチュアル・プロパティー・インコーポレイテッド Improved cooling system for commercial aircraft galleys.
US20050210910A1 (en) * 2004-03-29 2005-09-29 Rigney Richard N Cooling system for a commercial aircraft galley
AU2005228435B2 (en) * 2004-03-29 2010-11-11 Be Intellectual Property Inc. Improved cooling system for a commercial aircraft galley
US7231778B2 (en) 2004-03-29 2007-06-19 Be Intellectual Property, Inc. Cooling system for a commercial aircraft galley
US20060053831A1 (en) * 2004-09-10 2006-03-16 Serge Dube Evaporation circuit for alternative refrigerant in a refrigeration system
US8245769B2 (en) 2005-04-25 2012-08-21 Be Intellectual Property, Inc. Refrigerator-oven combination for an aircraft galley food service system
US9664422B2 (en) 2005-04-25 2017-05-30 Be Intellectual Property, Inc. Refrigerator-oven combination for an aircraft galley food service system
US7721797B2 (en) 2005-04-25 2010-05-25 Be Intellectual Property, Inc. Refrigerator-oven combination for an aircraft galley food service system
US20100200555A1 (en) * 2005-04-25 2010-08-12 Be Intellectual Property, Inc. Refrigerator-oven combination for an aircraft galley food service system
US8701752B2 (en) 2005-04-25 2014-04-22 Be Intellectual Property, Inc. Refrigerator-oven combination for an aircraft galley food service system
US7401473B2 (en) * 2005-09-26 2008-07-22 Systems Lmp Inc. Dual refrigerant refrigeration system and method
US20070068187A1 (en) * 2005-09-26 2007-03-29 Gaetan Lesage Dual refrigerant refrigeration system and method
CN101548140B (en) * 2006-10-23 2012-09-26 拉尔夫·慕斯卡泰尔 Solar air conditioning system
US20090032215A1 (en) * 2006-10-23 2009-02-05 Ralph Muscatell Water tank for use with a solar air conditioning system
WO2008051832A3 (en) * 2006-10-23 2008-10-23 Ralph Muscatell Solar air conditioning system
US7451611B2 (en) * 2006-10-23 2008-11-18 Ralph Muscatell Solar air conditioning system
US20080092575A1 (en) * 2006-10-23 2008-04-24 Ralph Muscatell Solar air conditioning system
GB2456693A (en) * 2006-10-23 2009-07-29 Ralph Muscatell Solar air conditioning system
US8292192B1 (en) 2008-07-01 2012-10-23 The United States Of America As Represented By The Secretary Of Agriculture Variable stage humidity control system for poultry hatcheries
US10040556B2 (en) 2013-10-07 2018-08-07 B/E Aerospace, Inc. Chilled air plenum system for aircraft galleys
US20170142939A1 (en) * 2015-11-24 2017-05-25 Incubation Systems, Inc. Egg incubator conversion kit
US10485223B2 (en) * 2015-11-24 2019-11-26 Incubation Systems, Inc. Egg incubator conversion kit
US20240278623A1 (en) * 2023-02-17 2024-08-22 GM Global Technology Operations LLC Multimodal cooling systems including integrated cooling devices with refrigerant-to-coolant heat exchangers

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